DE69511836T2 - Bremsklappe mit verstellbarem Spalt für einen Flugzeugflügel - Google Patents

Bremsklappe mit verstellbarem Spalt für einen Flugzeugflügel

Info

Publication number
DE69511836T2
DE69511836T2 DE69511836T DE69511836T DE69511836T2 DE 69511836 T2 DE69511836 T2 DE 69511836T2 DE 69511836 T DE69511836 T DE 69511836T DE 69511836 T DE69511836 T DE 69511836T DE 69511836 T2 DE69511836 T2 DE 69511836T2
Authority
DE
Germany
Prior art keywords
airplane wing
adjustable gap
brake flap
flap
brake
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE69511836T
Other languages
English (en)
Other versions
DE69511836D1 (de
Inventor
Danilo Ciprian
Benoit Hemadou
Pascal Chaumel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Publication of DE69511836D1 publication Critical patent/DE69511836D1/de
Application granted granted Critical
Publication of DE69511836T2 publication Critical patent/DE69511836T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B64C9/323—Air braking surfaces associated with wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Braking Arrangements (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Invalid Beds And Related Equipment (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Body Structure For Vehicles (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
DE69511836T 1994-12-26 1995-12-21 Bremsklappe mit verstellbarem Spalt für einen Flugzeugflügel Expired - Lifetime DE69511836T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9415641A FR2728535A1 (fr) 1994-12-26 1994-12-26 Aerofrein a fente variable pour voilure d'aeronef

Publications (2)

Publication Number Publication Date
DE69511836D1 DE69511836D1 (de) 1999-10-07
DE69511836T2 true DE69511836T2 (de) 2000-04-13

Family

ID=9470237

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69511836T Expired - Lifetime DE69511836T2 (de) 1994-12-26 1995-12-21 Bremsklappe mit verstellbarem Spalt für einen Flugzeugflügel

Country Status (7)

Country Link
US (1) US5735485A (de)
EP (1) EP0719704B1 (de)
CN (1) CN1065193C (de)
CA (1) CA2165513C (de)
DE (1) DE69511836T2 (de)
ES (1) ES2138171T3 (de)
FR (1) FR2728535A1 (de)

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FR2840877B1 (fr) * 2002-06-13 2004-08-06 Airbus France Dispositif d'articulation d'un volet sur une surface aerodynamique d'aeronef
US7258308B2 (en) * 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
US7243881B2 (en) * 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US6843452B1 (en) * 2003-06-17 2005-01-18 The Boeing Company Variable trailing edge geometry and spanload control
FR2859976B1 (fr) * 2003-09-22 2006-12-08 Airbus France Aile d'aeronef comportant au moins un volet deporteur et volet deporteur pour ladite aile
US6799739B1 (en) * 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7424350B2 (en) * 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US7270305B2 (en) * 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
FR2873094B1 (fr) * 2004-07-16 2008-01-18 Airbus France Sas Procede et dispositif d'amelioration de la manoeuvrabilite d'un aeronef lors des phases d'approche avant l'atterrissage puis d'arrondi
JP5184884B2 (ja) * 2004-07-16 2013-04-17 エアバス オペラシオン ソシエテ パ アクシオンス シンプリフィエ 着陸前の進入段階とその後の機首引き起こしの際に航空機の操縦性を改善する方法と装置
US7494094B2 (en) * 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) * 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
DE102004049504A1 (de) * 2004-10-11 2006-04-13 Airbus Deutschland Gmbh Flugzeugflügel, Verfahren zum Betreiben eines Flugzeugflügels und Verwendung einer schwenkbaren Hinterkante an einem Hauptflügel eines Flugzeugflügels zum Justieren der Form und Breite eines Luftspalts
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ES2277715B1 (es) * 2004-12-31 2008-05-16 Airbus España, S.L. Tapa reforzada para escotaduras en un contorno aerodinamico.
US7322547B2 (en) * 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) * 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
DE102005016578A1 (de) * 2005-04-11 2006-10-19 Airbus Deutschland Gmbh Einfachspaltklappe mit gleitender Abweiserklappe und absenkbarem Spoiler
US7721999B2 (en) * 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7500641B2 (en) * 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
US7611099B2 (en) † 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
DE102005045759A1 (de) * 2005-09-23 2007-04-12 Airbus Deutschland Gmbh Fortschrittlicheflügelhinterkante am Flügel eines Flugzeugs
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US7475854B2 (en) * 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US7578484B2 (en) * 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
DE102006030315A1 (de) * 2006-06-30 2008-01-17 Airbus Deutschland Gmbh Hochauftriebssystem am Tragflügel eines Flugzeugs
DE102006058561B4 (de) * 2006-12-12 2010-08-26 Hs Genion Gmbh Funktionseinrichtung mit schwenkbarem Element
DE102006059724B4 (de) * 2006-12-18 2011-03-17 Hs Genion Gmbh Luftleitvorrichtung für ein Fahrzeug
DE102007009060A1 (de) * 2007-02-23 2008-08-28 Airbus Deutschland Gmbh Spoiler für eine aerodynamisch wirksame Fläche eines Luftfahrzeugs
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) * 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8231079B2 (en) * 2008-03-31 2012-07-31 Honda Patents & Technologies North America, Llc Aerodynamic braking device for aircraft
DE102008020654B4 (de) 2008-04-24 2018-10-04 Airbus Operations Gmbh Tragflügel und Flugzeug mit einer Lateral-Kopplungsvorrichtung
IT1390909B1 (it) * 2008-07-16 2011-10-19 Alenia Aeronautica Spa Elemento strutturale a rigidezza calcolata, con caratteristiche di assorbimento di spostamenti e copertura interstizi
EP2174867A1 (de) * 2008-10-10 2010-04-14 Technische Universität München Vorrichtung zum Erzeugen von aerodynamischem Widerstand an einem Luftfahrzeug
GB0911012D0 (en) * 2009-06-25 2009-08-12 Airbus Operations Ltd Cross-bleed dam
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
CN102574575B (zh) * 2009-09-09 2015-09-30 威罗门飞行公司 一种航空飞行器
US8857761B2 (en) 2010-10-27 2014-10-14 Ata Engineering, Inc. Variable geometry aircraft pylon structure and related operation techniques
ES2602122T3 (es) * 2011-06-16 2017-02-17 Saab Ab Cubierta de doble curvatura para cubrir un hueco entre dos porciones estructurales de una aeronave
US9567867B2 (en) 2011-09-14 2017-02-14 Ata Engineering, Inc. Methods and apparatus for deployable swirl vanes
CN102540961B (zh) * 2012-01-10 2013-11-13 上海庞丰交通设备科技有限公司 基于plc控制的空气动力制动控制系统
US9108715B2 (en) * 2012-05-29 2015-08-18 The Boeing Company Rotary actuated high lift gapped aileron
CN103448902A (zh) * 2012-05-29 2013-12-18 中国航空工业集团公司西安飞机设计研究所 一种下单翼飞机的应急断离结构的内襟翼支臂梁及应用
IL226859A (en) * 2013-06-10 2017-09-28 Abramov Danny Slot wing with groove and wings for aircraft
CN104166348B (zh) * 2014-08-07 2016-08-17 北京理工大学 一种单滑块变质心控制飞行器的动态稳定性判定方法
GB201522486D0 (en) 2015-12-21 2016-02-03 Airbus Operations Ltd Seal assembly
EP3187413B1 (de) * 2015-12-30 2019-07-03 Airbus Defence and Space GmbH Flugzeugflügel mit spoiler
US11286032B2 (en) * 2019-08-30 2022-03-29 The Boeing Company Butterfly folding fairing
US11548616B1 (en) 2020-03-02 2023-01-10 Lucas Kai-Luen Hung Split-flap wing assembly for a high endurance aircraft
WO2022182427A1 (en) * 2021-02-23 2022-09-01 Barry Andersen Apparatus and method for a skirt assembly
GB2605195B (en) 2021-03-26 2023-12-13 Airbus Operations Ltd Trailing edge panel support with movable connector
GB2605196B (en) * 2021-03-26 2024-01-10 Airbus Operations Ltd Trailing edge panel support
GB2605194B (en) 2021-03-26 2023-12-13 Airbus Operations Ltd Trailing edge panel support with biasing arrangement
FR3143005A1 (fr) * 2023-07-07 2024-06-14 Airbus Operations (S.A.S.) Aéronef comprenant au moins un aérofrein présentant au moins deux parties mobiles entre elles

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Also Published As

Publication number Publication date
ES2138171T3 (es) 2000-01-01
FR2728535A1 (fr) 1996-06-28
EP0719704B1 (de) 1999-09-01
CA2165513A1 (fr) 1996-06-27
DE69511836D1 (de) 1999-10-07
CN1130140A (zh) 1996-09-04
CA2165513C (fr) 2009-04-07
CN1065193C (zh) 2001-05-02
US5735485A (en) 1998-04-07
FR2728535B1 (de) 1997-03-07
EP0719704A1 (de) 1996-07-03

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